LEADER 02083nam  2200553I  450 
001 9910705296503321
005 20140604094606.0
035   $a(CKB)5470000002448397
035   $a(OCoLC)880930822
035   $a(EXLCZ)995470000002448397
100   $a20140604j201308    ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor /$fRichard F. Bozak, Christopher E. Hughes, James Buckley
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dAugust 2013.
215   $a1 online resource (8 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2013-218066
300   $aTitle from title screen (viewed June 4, 2014).
300   $a"August 2013."
300   $a"Prepared for the Turbo Expo 2013 sponsored by the American Society of Mechanical Engineers (ASME) San Antonio, Texas, June 3-7, 2013."
300   $a"GT2013-95114."
320   $aIncludes bibliographical references (pages 7-8).
606   $aAcoustic properties$2nasat
606   $aAerodynamic noise$2nasat
606   $aBlade tips$2nasat
606   $aOscillating flow$2nasat
606   $aPressure ratio$2nasat
606   $aTurbofans$2nasat
606   $aRotors$2nasat
615  7$aAcoustic properties.
615  7$aAerodynamic noise.
615  7$aBlade tips.
615  7$aOscillating flow.
615  7$aPressure ratio.
615  7$aTurbofans.
615  7$aRotors.
700   $aBozak$b Richard F.$01405259
702   $aHughes$b Christopher E.
702   $aBuckley$b James$c(Mechanical engineer),
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705296503321
996   $aThe aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor$93520689
997   $aUNINA